Q-7: Assuming the following component efficiencies and ISA conditions pa = 0.4bar and Ta = 280 K, Calculate the propelling nozzle area required, net thrust developed and the SFC. (Assume QR = 42 MJ/kg). Isentropic efficiency of compressor and turbine = 87% Isentropic efficiency of intake & propelling nozzle = 98% Combustion chamber pressure loss = 4% of compressor deliver pressure.

Q-7: Assuming the following component efficiencies and ISA conditions pa = 0.4bar and Ta = 280 K, Calculate the propelling nozzle area required, net thrust developed and the SFC. (Assume QR = 42 MJ/kg). Isentropic efficiency of compressor and turbine = 87% Isentropic efficiency of intake & propelling nozzle = 98% Combustion chamber pressure loss = 4% of compressor deliver pressure.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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